JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5753' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5753' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2022070504653None · noneSHIP 3226 CORROSION IN FLAP ROTARY ACTUATOR TRACK 2 ON RH WING. CORRECTIVE ACTION: R/R ROTARY ACTUATOR PER DELTA WORKCARD AMDS 2754-4001-RT. (2300645)SDR SWAA2022070124435Flap · delaminatedRIGHT WING O/B AFT DELAMINATED I/B TRAILING EDGE. UPPER SURFACE APPROX 5.50' W X 6.0' LONG FROM TRAILING EDGE. TRAILING EDGE SPLIT. / [01] REMOVED AND REPLACED R/H WING; O/B AFT FLAP IAW AMM 27-51-22. OPERATION CHECK REQUIRED;[02] REMOVED AND REPLACED R/H WINGSDR SWAA2022071223748Flap · delaminatedRT WING O/B AFT FLAP UPPER SURFACE HAS A DELAM 3' O/B FROM I/B END; 3' FWD OF T/E. / DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS ACCORDING TO SRM 57-53-01-1A-4; FIG. 102; PARA. 4.A.(5 FABRICATED REPLACEMENT CORE PLUG FROM BMS 4-4; TY 4-25NPA (LOT# 1095039); AND USDR FDEA202206271579Flap · delaminatedRH WING OUTBOARD FLAP WITH DELAMINATION ON LEADING EDGE WBL: 379. R.H. WING OUTBOARD FLAP ON LEADING EDGE, OUTER SKIN, WBL: 379 WAS REPAIRED I.A.W. B767 S.R.M. 57-53-01-2R PAGE 1-5 FIG 201 SHEET 1, 3, 5 AND S.R.M. 51-70-17-0G FIG 10 SHEET 1 PARA. 4.A. PAGESDR FDEA202206271578Flap · delaminatedRH WING OUTBOARD FLAP L.E. NEAR TO IB EDGE - PREVIOUSLY REPAIR DELAMINATED. R.H. WING OUTBOARD FLAP L.E. NEAR TO INBD EDGE, OUTER SKIN WAS REPAIRED I.A.W. B767 S.R.M. 57-53-01-2R PAGE 1-5 FIG 201 SHEET 1, 3, 5 AND S.R.M. 51-70-17-0G FIG 10 SHEET 1 PARA. 4.SDR DALA2022070104590None · noneSHIP 3116 - CORROSION ON NUTS OF INTERCONNECTING STRUT IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED NUTS OF INTERCONNECTING STRUT IB FLAP ON RH WING AS PER A320 FAM AMM 27-51-44(2293759)SDR DALA2022070104589None · noneSHIP 3116 - CORROSION ON ON NUTS OF INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED NUTS OF INTERCONNECTING STRUT OB FLAP ON LH WING AS PER A320 FAM AMM 27-51-44(2293766)SDR DALA2022062804511Skin · corrodedSHIP 679 CORROSION ON UPPER SKIN OF INBD MAIN FLAP MFSTA. 220 APPROX AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00114: UPPER SKIN OF INBD MAIN FLAP MFSTA. 220 APPROX WAS REPAIRED PER B757-200 S.R.M. (2292292)SDR LR7A2022062403166Skin · dentedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH OUTBOARD FLAP UPPER SKIN DENTED AT 18 INCHES FROM THE TRAILING EDGE AT OWFS154.6L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1000701363.SDR LR7A2022062403158Baffle · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP BAFFLE UPPER SURFACE TRAILING EDGE CRACKED AT 6 INCHES FROM THE TRAILING EDGE AND 6 INCHES FROM THE INBOARD EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 100069212SDR LR7A2022062403157Baffle · crackedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH OUTBOARD FLAP BAFFLE LEADING EDGE UPPER SKIN CRACKED AT OWFS6L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1000692106.SDR LR7A2022062403153Skin · crackedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH OUTBOARD FLAP UPPER SKIN CRACKED AT OWFS136L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1000692035.SDR LR7A2022062403150Fastener · looseDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5712, FOUND THE RH INBOARD FLAP LOWER SKIN WITH SEVERAL LOOSE OR ERODED FASTENERS AT CWS183R, 14 INCHES FROM THE LEADING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 57-70-10. NR# 1000691428.SDR LR7A2022062403139Fastener · looseDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP LOWER SKIN WITH LOOSE FASTENERS 10" TO 16" FROM THE TRAILING EDGE AT OWFS125L. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1000688633.SDR UIEA2022062400669Skin · crackedLH INBD AILERON, OUTBD EDGE T/E SKIN CRACK AND CHAFING WORN PERFOM LH WING INBD AILERON OUTBD EDGE T/E WEDGE SKIN REPAIR. REFER O J/C ATTACHING SHEET 0307587. 2) CONDITION CHECK IS SATISFACTORY</P>)SDR IPXA2022070183676Stiffener · crackedINSPECTION TYPE:3CRH I/B WING T/E REAR SPAR VERTICAL STIFFENER CRACK FWD OF I/B AILERON.REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR)SDR AALA202206241190Fairing · puncturedAIRCRAFT IN BASE MAINTENANCE: RIGHT FLAP TRACK FAIRING NUMBER 6 HAS A SMALL PUNCTURE ON LOWER IN BOARD SIDE 5 INCHES FROM LEADING EDGE. ACCOMPLISHED PERMANENT REPAIR AT RIGHT FLAP-TRACK FAIRING NUMBER 6 IN BOARD SIDE PER B777-200 SRM 57-53-70-1A-1.SDR AALA202207065917Flap · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP LOWER SURFACE DEBONDED BETWEEN FLAP RIB 10 AND FLAP RIB 11. REPAIRED FLAP PER EA 336948.SDR DALA2022072005004Strut · corrodedSHIP 3229 CORROSION INTERCONNECTING STRUT OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER A320 AMM 27-51-44 AND 27-51-44. (2281248)SDR FDEA202206171462Flap · dentedRH WING INBOARD FLAP (AFT) LOWER SKIN WITH DENT AT WBL: 169. RH WING IBOARD AFT FLAP, LOWER SKIN AT WBL 169 WAS REPAIRED IAW B767 SRM 57-53-01- 2R PAGE 4 FIG. 201 SHEET 4 AND SRM 51-70-10-2R REP 4, PAGE 149-150 FIG 201 SHEET 1 REV. 82 12-15-21SDR FDEA202206171461Skin · gougedRIGHT WING OUTBOARD FLAP UPPER SKIN PANEL GOUGED REPAIRED RIGHT WING OUTBOARD FLAP UPPER SKIN PANEL IAW B757 SRM 57-53-01-2R-1 AND 51-70-10-2R REPAIR 4SDR FDEA202206171460Wedge · delaminatedR/W I/B FWD FLAP LOWER SURFACE T/E WEDGE IS DELAMINATED REMOVED AND REPLACED WEDGE PER BOEING DWG # 113N2603SDR DALA2022061704237Strut · corrodedSHIP 3229 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: R/R INTERCONNECTING STRUT. (2281245)SDR SWAA2022070719595Flap · delaminatedL/H WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD LOWER SURFACE L/H WING OUTBOARD AFT FLAP DELAMINATED ON INBOARD LOWER SURFACE. / [01] REMOVED L/H OUTBOARD AFT FLAP PER AMM 57-51-22.;[02] RII: INSPECTED THE WORK PERFORMED ON C/A #1; NO DEFECTS NOTED.;[03] UPDSDR CALA2022061701518Flap · inflt separationPDA 1 RIGHT I/B AFT FLAP HAS A SECTION MISSING APPROXIMATELY 15 1/2 INCHES BY 60 INCHES. PER GMM 02-30-95, THIS CLASSIFY AS CATEGORY 1 PDA. FLAGGED AS SDR, SENT INFO TO ESC PER GMM 02-30-95 ACP MATING SURFACE INSPECTION AND PART NUMBER VERIFICATION, OK TO INSTSDR SWAA2022081719114Support Angle · crackedLEFT WING IB UPPER FIXED TE PANEL SUPPORT ANGLE/SEAL RETAINER CRACKED AT ORSS 265; AFT / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED LEFT WING IB UPPER TE PANEL SUPPORT/SEAL RETAINER ORSS 265 AFT; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARSDR SWAA2022061618710Closeout Panel · crackedCLOSEOUT WEB UNDER LEFT WING PANEL 551GB CRACKED / [01] REMOVED AND REPLACED WEB REF SRM 51-40-02.SDR UIEA2022060800575Flap · dentedLH WING O/B FLAP FOUND DENT(PERFORMED REPAIR AT DENT AREA PER SRM 51-70-04 REPAIR 1)SDR VNAA202206099998Fitting · chafedLH O/B FLAP AT WS 178 AFT HINGE POINT FITTING ON WING HAS CHAFING ON METALSDR VNAA202206099992Skin · chafedL/H INBD FLAP INNER SKIN IS CHAFFED UNDER PANEL 584DBSDR REXA2022070701471Panel · chafedRHIB FLAP ACCESS PANEL 684EB CHAFED .023" DEEP, THIS IS BEYOND SRM LIMITS REPLACED ACCESS PANEL 684EBSDR SWAA2022061316301Web · crackedLH WING TRAILING EDGE DEFLECTION PANEL WEB ANGLE CRACKED. / [01] INSTALLED LH WING TRAILING EDGE DEFLECTION PANEL WEB ANGLE IAW SRM 51-40-02;[02] INSTALLED LH WING TRAILING EDGE DEFLECTION PANEL WEB ANGLE IAW SRM 51-40-02SDR IPXA2022070183678Hinge · brokenINSPECTION TYPE:3CL/H WING LWR REAR SPAR FLAP HINGE SUPPORT TENSION STRAP FOUND CRACKED.REMOVED, FABRICTED AND REPLACED HINGE SUPPORT IAW VT-SAA EA 011-5753-01-A9613 REV I/R AND UPS EO MD11-5720-84043-A FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) DATED 06/28/SDR IPXA2022062883590None · damagedINSPECTION TYPE:3CR/H I/B FLAP LOWER SKIN IS DENTED AT STA. YIFH= 41 AND BETWEEN XIFH= 255.59 AND XIFH= 261.69.REPAIRED DAMAGED R/H IB FLAP LOWER SKIN AT STA. YIFH= 41 AND BETWEEN XIFH= 255.59 AND XIFH= 261.69 IAW VT-SAA EA 011-5753-01-A9611 REV. I/R AND UPS ESDR LR7A2022060703116Skin · crackedDURING N401LC SCHEDULED A-1 CHECK UNDER JOB CARD HA1201, FOUND THE RH OUTBOARD FLAP TRAILING EDGE UPPER SKIN CRACKED IN TWO SPOTS AT OWFS64.5R, 6" - 12" FROM THE T.E.; REQUIRING MAJOR REPAIR. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12, AND BLIND FASTSDR JR2R20220606324Flap · damagedLH I/B AFT FLAP LOWER SURFACE DAMAGEDSDR SWAA2022071115497Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SKIN AT LT WING 2022-307300 / [01] TOOL USED; CALIPER PN: 500-464; SN: 15331926; DUE DATE: 28/SEP/22.;[02] TOOL USED; CALIPER PN: 500-197-30; SN: A21143429; DUE DATE: 11/OCT/22.;[03] TOOL USED: AUDIBLESDR DALA2022062204352Strut · corrodedSHIP 3230 CORROSION INTERCONNECTING STRUT OB FLAP ON RH WING . CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH PER DELTA WORKCARD AMDS CARD 2750-6010-RT. (2265543)SDR DALA2022060603918Strut · corrodedSHIP 3230 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: R/R INTERCONNECTING STRUT PER A320 AMM 27-51-44. OK FOR SERVICE. (2265539)SDR FDEA202206041375Flap · delaminatedRIGHT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION WBL: 414. RIGHT WING OUTBOARD FLAP LEADING EDGE WBL 414 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP. 1 PAG. 1-9 FIG. 201 (SHEET 5) TABLE I AND B767 SRM 51-70-17-0G PAR. 4.A. FIG. 10 REV. 82 DEC15/2021SDR SWAA2022060714550Seal Bracket · crackedLEFT WING UPPER FIXED TRAILING EDGE PANEL AFT OF #1 ENGINE FAIRING COVE SEAL RETAINER CRACKED. / [01] REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-40-02.;[02] INSPECTED WORK PERFORMED.SDR AALA202206075386Strut · wornAIRCRAFT IN BASE MAINTENANCE RIGHT WING INBOARD TRAILING EDGE FLAP INBOARD SIDE OF FLAP, STRUT ASSEMBLY - TORSION FOR TRUNNION ASSEMBLY WORN. REPLACED STRUT ASSEMBLY - TORSION FOR TRUNNION ASSEMBLY PER CMM 57-52-23.SDR SWAA2022061514637Flap · delaminatedL/H O/B AFT FLAP; I/B T/E CORNER; UPPER SURFACE DELAM. / [01] EVALUATED LH OB AFT FLAP; DELAMINATION IS REPAIRABLE IAW B737 SRM 57-53-01-2R-4. REMOVED DELAMINATED UPPER SKIN; CLEANED AND PREPPED AREA IAW B737 SRM 51-70-10-2R-4 PAR 3 AND SRM 51-70-10-2R-0 REPAISDR SWAA2022061517358Flap · delaminatedLEFT OUTBOARD AFT FLAP INBOARD UPPER CORNER DELAMINATED. / [01] LEFT OUTBOARD AFT FLAP INBOARD UPPER CORNER REPAIRED ON NR #TTG8Q00CTRHE;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR FDEA202205281319Wedge · damagedRIGHT WING INBOARD AFT FLAP TRAILING EDGE DAMAGED REPAIRED RIGHT WING INBOARD AFT FLAP TRAILING EDGE IAW B767 SRM 57-53-01-2R FIG 201 SHEET 4 REPAIR 1 AND 51-70-10-2R.SDR SWAA2022072112042Support Angle · elongatedELONGATED HOLE ON SUPPOR ANGLE TRAILING EDGE ORSS 251 LT WING 2022-274658 / [01] REPLACED SUPPOR ANGLE LOC.TRAILING EDGE ORSS 251 LT WING IAW B737-700 SRM 51-10-02 ITEM 9. PART USED P/N: 115A2350-1 P/O: 2021 769460.;[02] REPLACED SUPPOR ANGLE LOC.TRAILING EDGESDR FDEA202205241285Skin · delaminatedRH WING INBOARD FLAP (MAIN) LEADING EDGE DELAMINATION WBL: 276. RH WING INBOARD FLAP (MAIN) LEADING EDGE WBL:276 WAS REPAIRED IAW B767 SRM 57-53- 01-2R REPAIR 1 TABLE 1 FIG 201 AND B767 SRM 51-70-17-0G PAR. 4.B. FIG 24 REV. 82 DEC15/2021SDR AALA202207063649Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP RIB 15 FITTING. REPAIRED FITTING PER EA 336747.SDR SWAA2022052509394Bracket · crackedI/B T/E SUPPORT BRACKET FOR PANEL 551EB L/H WING IS CRACK. / [01] REMOVED I/B TRAILING EDGE SUPPORT BRACKET FOR ACCESS PANEL 551 EB AS PER BOEING 737 SRM 51-40-02;[02] VERIFIED STEP 1.;[03] CORRECTION: REMOVED AND REPLACED I/B TRAILING EDGE SUPPORT BRACKET(CLISDR SWAA2022061309119Flap · delaminatedR/H WING O/B AFT FLAP LOWER SURFACE I/B CORNER HAS AREA OF DELAM / [01] BOND TEST IAW B737 NDT PART 4; 51-00-05. DISBONDED AREA MARKED IN BLACK. TOOL#40082; DUE 11OCT22;[02] EVALUATED AND FOUND DELAMANATION AS MARKED. FOUND TO BE REPAIRABLE IAW SRM 57-53-01-2R
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